The starting, respectively the kindling in the two combustion chambers reactive to the constant pressure is achieved through the training in the contrary direction of the two turning platform (12) respectively (13) by an auxiliary engine source that can be mechanically or electrically. After the successive achievement of the minimal revolution (n_min) progressively enlarges under the control from the binnacle the pressure in the two standardised hydraulic circuits and integrated from the platforms (12) and (13), the fact that lead to apparition and the always progressive increase and controlled of the centrifugal forces generated by all the sectors of the circular crowns that compose the two turning platform (12) and (13).

That situation determines and can concomitantly guide to the la progressive reduction to the annulment of the gravitation influence. That phenomenon that is correlated with the phenomenon of specific pressure reducing uniformly distributed from the useful surface of the superior carcass (25) and correlated also with the two forces of traction of a same direction and diameter opposed generated by the two reactive combustion chamber (4), respectively (5), this proceeding determines together the detachment from the earth at fix point.

The manageability in the left and in the right direction of the displacement is achieved like I mentioned, through the power control respectively through the dozing of the two forces of traction, equal, diametrically opposed and of the same direction, generated by the reactive combustion chamber (4) respectively (5), by the dozing and under the permanent control from the binnacle, respectively the increase or the reducing of one of them having as direct consequence the change of the direction of flight towards the left or towards the right.

The management on the vertical to the up and to the bottom relatively to the direction of the flight, are also achieved very easy through the rotation of the horizontal axis (x-x) to an angle until (90) degrees, the axis that passes through the weight centre of the two combustion chamber (4) respectively (5), the manageability that can achieve with the help of some deflectors that change according to the desire of the running of the burning gases that leave with a big speed the spout (efuzors) of the two combustion chambers (4) respectively (5).

After what, acting identically as the manipulation left-right make the rising or the rapid descent of the whole system by this proceeding.

The proceeding that can be concomitantly superposed with the proceeding of the inertial displacement in zigzag previously described that the both superposed and harmoniously combined guide to the obtention of some exceptional performances very difficult to equal but not impossible as well as I will show and present further through another application of invention licence.

During the flight on the trajectory, it appears a trend of rotation uncontrolled of the horizontal axis (x-x) of the horizontal plan due to a generated couple of reactive combustion chambers (4) respectively (5) [that concomitantly also determines the rotation of the turning platforms (12) respectively (13)] the direction the burning gases being oriented below a small angle, down to the blades (11) of turbines, respectively of the combustion chamber (5) and on top to the blades of the turbine (10).

This trend is nevertheless counteracted by the corresponding position of the two deflectors located at the exit of the gases from the two combustion chambers, also due to the big gyroscopic effect due to the rotation of the two turning platforms (12) respectively (13), the solving of that effect needs a bigger angle of deflecting of burning gases, the manipulations that are permanently under control from the cabin of command located in the binnacle.

The calculation of the parameters of the flight in case of the inertial displacement in zigzag, is based on the using of the kinetic energies (Ec) accumulated during the rotation of the two discoidal turning system, the liberation of those energies conserved and their transforming into a useful mechanical working, respectively into a supplementary force of traction in the horizontal plan, being possible through the instantaneous displacement forced and successive of the instantaneous centres of rotation located on the axis (z-z) on the other axis of rotation parallel (z1-z1) that successively passes by the coupling points of the sabots (S1) respectively (S2) that can be alternatively acted during the progressive accumulation of the kinetic energy (Ec) that proportionally increases in the same time with the increase of the revolutions of the turning platform.

Like this, through the successive and momentaneouse coupling of the sabots, irises a big lack of balance of the masses located in rotation (over the minimal revolution) which has as practical result a tangential successive throwing of the whole system towards the front due to the successive revolutions of a turning platform that suddenly tends to zero and the kinetic energy conserved in this turning platform tends also to be liberated suddenly (instantaneously) through the transforming also instantaneously under the useful mechanic work form (Lu)=(Ftsupl).(D), respectively into a supplementary force of traction (Ftsupl) on a distance(D) representing the crossed distance into a single zigzag, (according to the principle, of conservation, - nothing does not disappear, - nothing does not appears, - but everything is transformed)

The value of the kinetic energy liberate and transformed into a mechanic useful working, being proportional with <collapse> of the revolution in the interval of time necessary to the crossing of the distance (D), that supplementary force of traction guides to the supplementary and successive increase of the average speed of displacement of the whole system into a perpendicular plan on the rotation axis (z-z) can be calculated through the applying of the theorem of Steiner from the physics on the axis (z1-z1) respectively in the centre of the sabot S1 for the superior, and the centre of the sabots (S2) for the inferior turning system according to the relations:  where (I) represents the kinetic moment of the discoidal turning superior system opposite to the centre or to the relative rotation, located on the axis of communal symmetry (z-z), (I1) represents the kinetic moment superior turning system, face to a centre of rotation relatively located on the vertical axis (z1-z1) situated at the distance (d) from the axis of vertical symmetry (z-z).

From the tables we know that by example for a cylindrical ring  where (R) is the exterior radius and (r) is the interior radius of the cylindrical ring, and (M) is the superior turning system mass.

Similarly the values in the case of coupling the symmetric sabot can be calculated (S2) and also similarly, knowing all those values the Theorem of Steiner can be used in order to calculate the kinetic energy with the help of the relation;  for the axis of rotation (z1-z1) respectively  where (w) is angular speed.

Applying successively that theorem and knowing a certain initial average speed of displacement of the whole system, the resultant trajectory being the axis of symmetry of <the steps> (the zigzags) and admitting the symmetric and valoricaly equal forces applied above the sabots (S1) and successive (S2), we can determine the gain of speed in a unit of time for a space equal to the step of one zigzag, respectively they can be calculated at the designing of the basis parameters in order to dimension correspondingly because D (Ec)=(LM)=(Ftsupl).(D) but, of course taking account at each time inertia and the influence of the stationary platform.

I mentioned that this proceeding of construction, displacement and functioning based on the principle of the moving by rotation of the bodies and of nature forces, is one of the proceedings universally available for the displacement and material communication between two celestial body of the observable universe that can be used by the intelligent beings, - but not the single.